# N886FD: 2012 Boeing 777-FS2

- Status: Valid registration
- Airframe: [Boeing 777-FS2](https://openairdocs.org/model/boeing-777-fs2) (registry code 138527H, 13 seats)
- Engine: [GE GE90-110B1](https://openairdocs.org/engine/ge-ge90-110b1) (registry code 30046)
- Data sheets: [TCDS E00049EN](https://openairdocs.org/tcds/E00049EN) (General Electric Company GE Aviation) (OpenAirDocs)
- Serial number: 41065
- Year built: 2012
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 31, 2012
- Certificate issued: September 5, 2012
- Expires: September 30, 2028
- Mode S code: AC34A0
- Registered owner: [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION)
- Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)
- Owner type: Corporation
- Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=886FD
- Page: https://openairdocs.org/aircraft/N886FD

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 21 in force

### Matched by airframe (Boeing 777-FS2)

None in force.

### Matched by engine (GE GE90-110B1)

- [AD 2025-25-07](https://openairdocs.org/ad/2025-25-07): Turbine Section · General Electric Company GE GE90-90B, GE90-94B, GE90-110B1 and 1 more. Effective Feb 6, 2026
- [AD 2025-07-10](https://openairdocs.org/ad/2025-07-10): Fuel Controlling System · General Electric Company GE GE90-110B1 and GE90-115B. Effective May 21, 2025
- [AD 2024-06-15](https://openairdocs.org/ad/2024-06-15): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective May 14, 2024
- [AD 2023-26-07](https://openairdocs.org/ad/2023-26-07): Turbine Section · General Electric GE90-90B, GE90-94B, GE90-110B1 and 1 more. Effective Feb 27, 2024
- [AD 2023-04-19](https://openairdocs.org/ad/2023-04-19): Turbine Engine Compressor Section · General Electric GE90-110B1 and GE90-115B. Effective Mar 27, 2023
- [AD 2022-23-09](https://openairdocs.org/ad/2022-23-09): Turbine Engine Compressor Section, Turbine Section · General Electric GE90-90B, GE90-94B, GE90-110B1 and 1 more. Effective Jan 17, 2023
- [AD 2022-18-06](https://openairdocs.org/ad/2022-18-06): Turbine Engine Compressor Section, Turbine Section · General Electric GE90-110B1, GE90-115B, GE90-76B and 3 more. Effective Oct 26, 2022
- [AD 2021-26-06](https://openairdocs.org/ad/2021-26-06): Turbine Engine Accessory Drive · General Electric GE90-76B, GE90-85B, GE90-90B and 3 more. Effective Feb 15, 2022
- [AD 2020-21-13](https://openairdocs.org/ad/2020-21-13): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective Nov 17, 2020
- [AD 2020-18-14](https://openairdocs.org/ad/2020-18-14): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective Oct 21, 2020
- [AD 2020-10-04](https://openairdocs.org/ad/2020-10-04): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective May 27, 2020
- [AD 2020-01-55](https://openairdocs.org/ad/2020-01-55): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective Mar 2, 2020
- [AD 2018-20-23](https://openairdocs.org/ad/2018-20-23): Turbine Engine Compressor Section · General Electric GE90-110B1 and GE90-115B. Effective Nov 30, 2018
- [AD 2018-20-22](https://openairdocs.org/ad/2018-20-22): Turbine Section · General Electric GE90-110B1, GE90-113B and GE90-115B. Effective Nov 13, 2018
- [AD 2017-08-06](https://openairdocs.org/ad/2017-08-06): Engine Oil Cooler · General Electric GE90-110B1, GE90-115B, GE90-76B and 3 more. Effective May 22, 2017
- [AD 2013-23-18](https://openairdocs.org/ad/2013-23-18): Variable bypass valve (VBV) actuator fuel supply tube · General Electric GE90-110B1 and GE90-115B. Effective Jan 7, 2014
- [AD 2013-17-07](https://openairdocs.org/ad/2013-17-07): Stage 1 high-pressure turbine (HPT) stator shrouds · General Electric GE90-110B1, GE90-115B, GE90-76B and 3 more. Effective Oct 18, 2013
- [AD 2013-15-20](https://openairdocs.org/ad/2013-15-20): Transfer gearbox assembly (TGB) radial gearshafts · General Electric GE90-110B1, GE90-113B, GE90-115B and 5 more. Effective Aug 21, 2013
- [AD 2011-26-11](https://openairdocs.org/ad/2011-26-11): HPC stages 1-2 seal teeth · General Electric GE90-110B1 and GE90-115B. Effective Feb 3, 2012
- [AD 2009-25-14](https://openairdocs.org/ad/2009-25-14): Blade · General Electric GE90-110B1, GE90-113B and GE90-115B. Effective Jan 19, 2010
- [AD 2007-10-05](https://openairdocs.org/ad/2007-10-05): Turbine Center Frames (TCFs) · General Electric GE90-110B1, GE90-113B and GE90-115B. Effective Jun 14, 2007

### Historical (superseded or no longer in force)

- [AD 2021-15-05](https://openairdocs.org/ad/2021-15-05) (historical): Engine Controls · General Electric GE90-110B1 and GE90-115B. Effective Sep 13, 2021
- [AD 2020-20-17](https://openairdocs.org/ad/2020-20-17) (historical): Engine Controls · General Electric GE90-110B1 and GE90-115B. Effective Oct 23, 2020
- [AD 2017-07-04](https://openairdocs.org/ad/2017-07-04) (historical): Compressor Section · General Electric GE90-110B1 and GE90-115B. Effective Apr 21, 2017
- [AD 2013-24-17](https://openairdocs.org/ad/2013-24-17) (historical): High pressure compressor (HPC) rotor stage 2-5 spools · General Electric GE90-110B1 and GE90-115B. Effective Dec 31, 2013
- [AD 2013-14-51](https://openairdocs.org/ad/2013-14-51) (historical): Failure of a transfer gearbox assembly radial gearshaft · General Electric GE90-110B1 and GE90-115B
- [AD 2013-10-52](https://openairdocs.org/ad/2013-10-52) (historical): Transfer gearbox assemblies (TGBs) · General Electric GE90-110B1 and GE90-115B. Effective Jun 26, 2013

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N886FD.

## FAA accident and incident reports

None matched to N886FD.

## Service difficulty reports (14)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR FDEA202602160216](https://openairdocs.org/sdr/FDEA202602160216), Feb 16, 2026: SAFETY WIRE. WRONG PART. FOUND L1 DOOR SLIDE SAFETY WIRE NON-COMPATIBLE, NEEDS REPLACING. REPLACED SAFETY WIRE WITH PART NO. MS20995CY16 CAD PLATED COPPER. REF. AMM 25-66-01-4. AC OK FO
- [SDR FDEA202602010111](https://openairdocs.org/sdr/FDEA202602010111), Feb 1, 2026: LIGHT. NO TEST. DURING PREFLT, EMERGENCY LIGHT TEST IN GALLEY, SMALL SQUARE LIGHT ABOVE L1 DID NOT ILLUMINATE IAW TEST REQUIREMENTS. REPLACED SMALL SQUARE LIGHT (AREA LIGHT) AS
- [SDR FDEA202511052126](https://openairdocs.org/sdr/FDEA202511052126), Nov 5, 2025: SKIN. DAMAGED. FOUND A LIGHTNING STRIKE DAMAGE AT RUDDER LH SURFACE AT RUD STA 487 & 4" FWD OF RUDDER TRAILING EDGE. REPAIRED A LIGHTNING STRIKE DAMAGE AT RUDDER LH SURFACE AT
- [SDR FDEA202410241580](https://openairdocs.org/sdr/FDEA202410241580), Oct 24, 2024: LAMP. INOPERATIVE. POST-FLT INSP, (1EA) SUPRMNRY OVRHD EMERGENCY LT INOP. AMM: 33-50-00-2 RE-LAMPED, REF B777 AMM: 33-50-00-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.
- [SDR FDEA202305160877](https://openairdocs.org/sdr/FDEA202305160877), May 16, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 FOUND CRACKED AT STA 1660 RBL1. EVALUATED THE MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 CRACKED AT STA 1660 RBL1.DAM
- [SDR FDEA202305160876](https://openairdocs.org/sdr/FDEA202305160876), May 16, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8650-4 FOUND CRACKED AT STA1780 RBL1. EVALUATED THE MAIN DECK CARGO FLOOR PANEL P/N:152W8650-4 CRACKED AT STA1780 RBL1 DAMAG
- [SDR FDEA202305160875](https://openairdocs.org/sdr/FDEA202305160875), May 16, 2023: FLAP. DENTED. LH OB FLAP LWR SURFACE FROM OB TO IB 10INCH CROSS TE TO LE 2.25INCH FOUND ONE DENT. EVALUATED LH OB FLAP LWR SURFACE FROM OB TO IB 10INCH CROSS TE TO LE 2.25INC
- [SDR FDEA202305160874](https://openairdocs.org/sdr/FDEA202305160874), May 16, 2023: FLAP. DENTED. LH OB FLAP LWR SURFACE FROM IB TO OB 3.8INCH CROSS TE TO LE 15.5INCH FOUND ONE DENT. EVALUATED LH OB FLAP LWR SURFACE FROM IB TO OB 3.8INCH CROSS TE TO LE 15.5I
- [SDR FDEA202305160873](https://openairdocs.org/sdr/FDEA202305160873), May 16, 2023: FLAP. DELAMINATED. LH OB FLAP LWR SURFACE FROM OB TO IB 124INCH CROSS TE TO LE 7INCH FOUND DELAMINATION . EVALUATED LH OB FLAP LWR SURFACE FROM OB TO IB 124INCH CROSS TE TO LE 7IN
- [SDR FDEA202208242044](https://openairdocs.org/sdr/FDEA202208242044), Aug 24, 2022: LAMP. INOPERATIVE. PRE-FLT MX INSP, (1) OVRHD EMERGENGY LT INOP SUPRNMRY AREA. RE-LAMPED, REF B777 AMM: 33-51-04-2. LT TESTS SATIS, ITEM OK FOR SVC.
- [SDR FDEA202008242000](https://openairdocs.org/sdr/FDEA202008242000), Aug 24, 2020: FLOOR SUPPORT. CRACKED. LOWER BULK CARGO COMPARTMENT FLOOR PANEL ATTACHMENT STRINGER FOUND CRACK AT STATION 1958 RBL 41.5. LOWER BULK CARGO COMPARTMENT FLOOR PANEL ATTACHMENT STRINGER 
- [SDR FDEA201901100084](https://openairdocs.org/sdr/FDEA201901100084), Jan 10, 2019: INDICATION SYS. MALFUNCTIONED. AIRCRAFT DIVERTED TO RKSI, DUE TO HIGHER THAN PLANNED FUEL BURN RATE. REVIEWED MAT, COULDN'T FIND ANY RELATED MSG, REVIEWED FMC AND INDICATED FUEL ONBOARD WAS 1
- [SDR FDEA201712303475](https://openairdocs.org/sdr/FDEA201712303475), Dec 30, 2017: SKIN. DENTED. LEFT WING NR 4 SLAT DENTED. REPAIRED THE LT WING NR 4 SLAT NOSE SKIN IAW SRM 57-43-01-2R, REPAIR.2, FIGURE.203. MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201405261196](https://openairdocs.org/sdr/FDEA201405261196), May 26, 2014: UNKNOWN. MALFUNCTIONED. ON TAKEOFF ROLL AT APROX 1100-120KTS ALL PERFORMANCE DATA DUMPED V1,VR DISAPPEARED SPEED DATA ONLY SHOWED V2 BECAUSE IT WAS SET IN SPEED WINDOW. COMMANDED ROTAT

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Boeing 777-FS2 aircraft: https://openairdocs.org/model/boeing-777-fs2/aircraft.md
- The GE GE90-110B1 engine: https://openairdocs.org/engine/ge-ge90-110b1.md

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